CFD-Based Aeroelastic Sensitivity Study of a Low-Speed Flutter Demonstrator

Titel:: CFD-Based Aeroelastic Sensitivity Study of a Low-Speed Flutter Demonstrator
Dokumenttyp:: Zeitschriftenaufsatz
Autor(en):: Rozov, Vladyslav; Volmering, Andreas; Hermanutz, Andreas; Hornung, Mirko; Breitsamter, Christian
Abstract:: The goal of developing aircraft that are greener, safer and cheaper can only be maintained through significant innovations in aircraft design. An integrated multidisciplinary design approach can lead to an increase in the performance of future derivative aircraft. Advanced aerodynamics and structural design technologies can be achieved by both passive and active suppression of aeroelastic instabilities.
Stichworte:: Antisymmetric boundary condition; Computational aeroelasticity; FLEXOP; Flutter analysis; Flutter demonstrator; Linearized CFD; SD-CFD; Sensitivity study; Stability analysis
Zeitschriftentitel:: Aerospace
Jahr:: 2019
Band / Volume:: 6
Heft / Issue:: 3
Seitenangaben Beitrag:: 30
Nachgewiesen in:: Scopus
Volltext / DOI:: doi:10.3390/aerospace6030030
WWW:: https://www.mdpi.com/2226-4310/6/3/30
Verlag / Institution:: MDPI AG
E-ISSN:: 2226-4310
Eingereicht (bei Zeitschrift):: 06.02.2019
Angenommen (von Zeitschrift):: 01.03.2019
Publikationsdatum:: 06.03.2019
TUM Einrichtung:: Lehrstuhl für Aerodynamik und Strömungsmechanik
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